FX 83-W-160 (fx83w160-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: FX 83-W-160 (fx83w160-il) Reynolds number: 500,000 Max Cl/Cd: 109.59 at α=5.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx83w160-il-500000.txt Download as CSV file: xf-fx83w160-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: FX 83-W-160
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.500 -0.7562 0.11278 0.10954 -0.0743 1.0000 0.0246
-18.250 -0.7868 0.10382 0.10042 -0.0788 1.0000 0.0247
-18.000 -0.8044 0.09768 0.09419 -0.0817 1.0000 0.0248
-17.750 -0.8195 0.09213 0.08855 -0.0842 1.0000 0.0250
-17.500 -0.8348 0.08677 0.08311 -0.0864 1.0000 0.0252
-17.250 -0.8468 0.08213 0.07840 -0.0883 1.0000 0.0254
-17.000 -0.8587 0.07770 0.07389 -0.0899 1.0000 0.0257
-16.750 -0.8717 0.07337 0.06947 -0.0912 1.0000 0.0259
-16.500 -0.8846 0.06931 0.06533 -0.0922 1.0000 0.0262
-16.250 -0.8967 0.06566 0.06159 -0.0929 1.0000 0.0265
-16.000 -0.9103 0.06220 0.05805 -0.0929 1.0000 0.0266
-15.750 -0.9231 0.05918 0.05494 -0.0927 1.0000 0.0268
-15.500 -0.9293 0.05578 0.05142 -0.0943 0.9995 0.0273
-15.250 -0.9224 0.05219 0.04769 -0.0982 0.9978 0.0276
-15.000 -0.9149 0.04868 0.04402 -0.1024 0.9958 0.0280
-14.750 -0.9049 0.04586 0.04117 -0.1053 0.9939 0.0287
-14.500 -0.8925 0.04335 0.03861 -0.1081 0.9912 0.0293
-14.250 -0.8777 0.04097 0.03617 -0.1113 0.9888 0.0298
-14.000 -0.8606 0.03872 0.03384 -0.1146 0.9869 0.0304
-13.750 -0.8450 0.03656 0.03158 -0.1174 0.9840 0.0311
-13.500 -0.8281 0.03458 0.02947 -0.1201 0.9802 0.0319
-13.250 -0.8071 0.03262 0.02739 -0.1233 0.9778 0.0326
-13.000 -0.7868 0.03057 0.02533 -0.1264 0.9762 0.0336
-12.750 -0.7732 0.02904 0.02377 -0.1274 0.9702 0.0343
-12.500 -0.7500 0.02750 0.02217 -0.1301 0.9675 0.0352
-12.250 -0.7229 0.02610 0.02067 -0.1333 0.9658 0.0365
-12.000 -0.7035 0.02490 0.01936 -0.1346 0.9609 0.0374
-11.750 -0.6868 0.02310 0.01754 -0.1363 0.9564 0.0387
-11.500 -0.6604 0.02180 0.01621 -0.1392 0.9540 0.0401
-11.250 -0.6292 0.02070 0.01503 -0.1423 0.9525 0.0418
-11.000 -0.6142 0.02000 0.01423 -0.1414 0.9454 0.0431
-10.750 -0.5884 0.01880 0.01303 -0.1433 0.9421 0.0453
-10.500 -0.5561 0.01805 0.01224 -0.1456 0.9400 0.0476
-10.250 -0.5229 0.01729 0.01140 -0.1479 0.9380 0.0502
-10.000 -0.5110 0.01670 0.01081 -0.1459 0.9300 0.0527
-9.750 -0.4810 0.01618 0.01024 -0.1472 0.9266 0.0557
-9.500 -0.4509 0.01552 0.00955 -0.1487 0.9237 0.0593
-9.250 -0.4297 0.01516 0.00918 -0.1480 0.9184 0.0626
-9.000 -0.4060 0.01478 0.00873 -0.1477 0.9133 0.0661
-8.750 -0.3784 0.01423 0.00819 -0.1484 0.9095 0.0707
-8.500 -0.3461 0.01384 0.00773 -0.1499 0.9065 0.0754
-8.250 -0.3311 0.01347 0.00740 -0.1478 0.9000 0.0801
-8.000 -0.3041 0.01321 0.00708 -0.1480 0.8957 0.0852
-7.750 -0.2762 0.01276 0.00665 -0.1486 0.8921 0.0925
-7.500 -0.2500 0.01250 0.00636 -0.1486 0.8879 0.0989
-7.250 -0.2286 0.01223 0.00611 -0.1477 0.8827 0.1059
-7.000 -0.2022 0.01194 0.00580 -0.1477 0.8786 0.1137
-6.750 -0.1731 0.01169 0.00554 -0.1483 0.8753 0.1227
-6.500 -0.1469 0.01140 0.00528 -0.1483 0.8715 0.1334
-6.250 -0.1247 0.01117 0.00507 -0.1474 0.8667 0.1435
-6.000 -0.0983 0.01093 0.00483 -0.1473 0.8625 0.1558
-5.750 -0.0702 0.01065 0.00457 -0.1477 0.8590 0.1707
-5.500 -0.0415 0.01037 0.00434 -0.1482 0.8556 0.1905
-5.250 -0.0200 0.01011 0.00418 -0.1472 0.8512 0.2145
-5.000 0.0051 0.00981 0.00398 -0.1469 0.8471 0.2443
-4.750 0.0320 0.00950 0.00378 -0.1471 0.8436 0.2836
-4.500 0.0607 0.00921 0.00362 -0.1476 0.8404 0.3277
-4.250 0.0856 0.00901 0.00353 -0.1472 0.8365 0.3643
-4.000 0.1102 0.00886 0.00347 -0.1466 0.8321 0.3972
-3.750 0.1376 0.00874 0.00341 -0.1466 0.8281 0.4252
-3.500 0.1671 0.00868 0.00336 -0.1469 0.8248 0.4478
-3.250 0.1977 0.00869 0.00335 -0.1475 0.8216 0.4660
-3.000 0.2218 0.00868 0.00338 -0.1467 0.8177 0.4802
-2.750 0.2486 0.00870 0.00342 -0.1465 0.8139 0.4933
-2.500 0.2773 0.00874 0.00345 -0.1466 0.8106 0.5069
-2.250 0.3072 0.00880 0.00345 -0.1470 0.8076 0.5182
-2.000 0.3384 0.00887 0.00350 -0.1477 0.8047 0.5267
-1.750 0.3628 0.00893 0.00355 -0.1469 0.8011 0.5349
-1.500 0.3891 0.00894 0.00359 -0.1465 0.7973 0.5413
-1.250 0.4176 0.00898 0.00361 -0.1466 0.7938 0.5490
-1.000 0.4471 0.00901 0.00363 -0.1469 0.7907 0.5566
-0.750 0.4784 0.00911 0.00371 -0.1476 0.7876 0.5645
-0.500 0.5020 0.00917 0.00377 -0.1466 0.7837 0.5715
-0.250 0.5281 0.00917 0.00383 -0.1462 0.7798 0.5775
0.000 0.5564 0.00920 0.00386 -0.1463 0.7762 0.5834
0.250 0.5863 0.00927 0.00387 -0.1467 0.7731 0.5889
0.500 0.6159 0.00928 0.00390 -0.1470 0.7697 0.5932
0.750 0.6392 0.00929 0.00397 -0.1460 0.7652 0.5975
1.000 0.6658 0.00930 0.00398 -0.1457 0.7603 0.6029
1.250 0.6951 0.00931 0.00395 -0.1459 0.7558 0.6077
1.500 0.7224 0.00932 0.00398 -0.1457 0.7513 0.6118
1.750 0.7453 0.00928 0.00399 -0.1446 0.7446 0.6156
2.000 0.7743 0.00924 0.00389 -0.1446 0.7368 0.6198
2.250 0.7936 0.00921 0.00387 -0.1427 0.7274 0.6240
2.500 0.8211 0.00918 0.00380 -0.1424 0.7195 0.6283
2.750 0.8421 0.00917 0.00388 -0.1409 0.7127 0.6324
3.000 0.8667 0.00919 0.00392 -0.1402 0.7069 0.6372
3.250 0.8944 0.00925 0.00395 -0.1401 0.7013 0.6419
3.500 0.9147 0.00925 0.00402 -0.1385 0.6937 0.6459
3.750 0.9398 0.00927 0.00403 -0.1378 0.6860 0.6497
4.000 0.9591 0.00929 0.00410 -0.1359 0.6766 0.6538
4.250 0.9827 0.00935 0.00414 -0.1349 0.6677 0.6582
4.500 1.0011 0.00939 0.00422 -0.1329 0.6571 0.6627
4.750 1.0203 0.00944 0.00430 -0.1310 0.6462 0.6672
5.000 1.0366 0.00951 0.00437 -0.1285 0.6338 0.6721
5.250 1.0510 0.00959 0.00446 -0.1257 0.6199 0.6774
5.500 1.0649 0.00972 0.00459 -0.1227 0.6037 0.6829
5.750 1.0758 0.00994 0.00478 -0.1192 0.5829 0.6890
6.000 1.0834 0.01025 0.00502 -0.1151 0.5543 0.6954
6.250 1.0849 0.01074 0.00536 -0.1099 0.5170 0.7018
6.500 1.0828 0.01140 0.00584 -0.1042 0.4736 0.7092
6.750 1.0788 0.01224 0.00646 -0.0985 0.4269 0.7175
7.000 1.0785 0.01305 0.00712 -0.0936 0.3871 0.7273
7.250 1.0783 0.01395 0.00786 -0.0890 0.3471 0.7391
7.500 1.0816 0.01478 0.00858 -0.0850 0.3120 0.7543
7.750 1.0859 0.01559 0.00932 -0.0813 0.2809 0.7756
8.000 1.0910 0.01632 0.01006 -0.0778 0.2546 0.8113
8.250 1.1169 0.01707 0.01093 -0.0790 0.2223 0.9731
8.500 1.1245 0.01786 0.01162 -0.0760 0.2046 1.0000
8.750 1.1365 0.01869 0.01236 -0.0740 0.1878 1.0000
9.000 1.1484 0.01953 0.01312 -0.0721 0.1737 1.0000
9.250 1.1606 0.02038 0.01389 -0.0702 0.1613 1.0000
9.500 1.1745 0.02115 0.01463 -0.0686 0.1506 1.0000
9.750 1.1879 0.02197 0.01541 -0.0670 0.1413 1.0000
10.000 1.2006 0.02284 0.01624 -0.0653 0.1327 1.0000
10.250 1.2149 0.02364 0.01703 -0.0639 0.1255 1.0000
10.500 1.2272 0.02457 0.01793 -0.0623 0.1182 1.0000
10.750 1.2415 0.02541 0.01878 -0.0610 0.1123 1.0000
11.000 1.2542 0.02635 0.01970 -0.0595 0.1061 1.0000
11.250 1.2670 0.02731 0.02066 -0.0581 0.1006 1.0000
11.500 1.2803 0.02825 0.02160 -0.0568 0.0952 1.0000
11.750 1.2912 0.02937 0.02271 -0.0553 0.0900 1.0000
12.000 1.3052 0.03031 0.02367 -0.0542 0.0853 1.0000
12.250 1.3146 0.03158 0.02491 -0.0526 0.0806 1.0000
12.500 1.3278 0.03261 0.02599 -0.0515 0.0769 1.0000
12.750 1.3387 0.03381 0.02719 -0.0502 0.0728 1.0000
13.000 1.3472 0.03524 0.02862 -0.0488 0.0693 1.0000
13.250 1.3601 0.03634 0.02978 -0.0478 0.0663 1.0000
13.500 1.3698 0.03771 0.03115 -0.0466 0.0630 1.0000
13.750 1.3769 0.03933 0.03279 -0.0453 0.0602 1.0000
14.000 1.3893 0.04053 0.03406 -0.0444 0.0575 1.0000
14.250 1.3982 0.04204 0.03558 -0.0434 0.0549 1.0000
14.500 1.4034 0.04392 0.03748 -0.0422 0.0526 1.0000
14.750 1.4145 0.04530 0.03893 -0.0414 0.0503 1.0000
15.000 1.4226 0.04698 0.04062 -0.0405 0.0479 1.0000
15.500 1.4335 0.05092 0.04467 -0.0387 0.0444 1.0000
15.750 1.4411 0.05275 0.04657 -0.0380 0.0428 1.0000
16.000 1.4457 0.05491 0.04876 -0.0373 0.0414 1.0000
16.250 1.4449 0.05768 0.05156 -0.0366 0.0399 1.0000
16.500 1.4503 0.05986 0.05383 -0.0361 0.0388 1.0000
16.750 1.4560 0.06202 0.05609 -0.0357 0.0377 1.0000
17.000 1.4600 0.06444 0.05858 -0.0354 0.0366 1.0000
17.250 1.4624 0.06709 0.06128 -0.0351 0.0356 1.0000
17.500 1.4602 0.07032 0.06454 -0.0350 0.0345 1.0000
17.750 1.4603 0.07333 0.06765 -0.0350 0.0337 1.0000
18.000 1.4639 0.07600 0.07044 -0.0351 0.0328 1.0000
18.250 1.4656 0.07895 0.07348 -0.0354 0.0320 1.0000
18.500 1.4661 0.08210 0.07671 -0.0358 0.0312 1.0000
18.750 1.4656 0.08546 0.08014 -0.0363 0.0306 1.0000
19.000 1.4613 0.08938 0.08412 -0.0371 0.0299 1.0000
19.250 1.4544 0.09364 0.08844 -0.0380 0.0293 1.0000
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